Registered owner
Bank Of Utah Trustee
Owner type
Corporation
Serial number
55172
Year built
2022
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 27, 2022
Certificate issued
October 27, 2022
Expires
October 31, 2029
Mode S code
A1CFFD

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 71

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2017In forceSuperseded2026
ADs by the year they took effect: 81 ADs
20171
20191
20204
202110
202211
202311
202417
202516
202610
See all 81 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N216BZMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus Canada LP BD-500-1A11 aircraft

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR BAGA2025111100001Engine · fireAFTER LANDING, AS CLEARING THE RUNWAY R ENG FIRE WARNING MSG. RAN THE R ENG FIRE CHECKLIST. ENGINE REMOVE AND REPLACE.Nov 9, 2025 · N216BZ · Airbus BD5001A11 · Engine (Turbine/Turboprop)SDR BAGA2025092400008Skin · corrodedHEAVY CHECK SUBMISSION, AFT CARGO DOOR LOWER SKIN CORROSION AROUND ATTACHMENT HOLES UNDERNEATH SCUFF PLATES, REPAIRED PER REO.Sep 23, 2025 · N216BZ · Airbus BD5001A11 · Cargo/Baggage DoorsSDR BAGA2025092400007Door Sill · corrodedHEAVY CHECK, FWD CARGO DOOR SILL FOUND CORROSION AROUND ATTACHMENT HOLES. REPAIRED PER REO.Sep 23, 2025 · N216BZ · Airbus BD5001A11 · Fuselage Main, StructureSDR BAGA2025092400006Skin · corrodedHEAVY CHECK, REAR FUSELAGE AT FR 79 LOWER SKIN FOUND CORRODED, REPAIRED PER REO.Sep 23, 2025 · N216BZ · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR BAGA2025092400005Doubler · corrodedAIRCRAFT IN HEAVY CHECK, REAR FUSELAGE WASTE DOUBLER FOUND CORROSION AT FR75/76. REAR FUSELAGE WASTE DOUBLER REPAIRED PER REO.Aug 26, 2025 · N216BZ · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR BAGA2024100100001Unknown · odorAT 36,000FT OVER THE MIDDLE OF KANSAS, FIRST FAULT WE NOTICED WAS THE COCKPIT DOOR FAULT. THE NEXT FAULT WAS FD FAULT, WHICH WAS TEMP AND WHEN IT CLEARED, ALL THE OTHER FAULTS APPEARED (SEE ATTACHED PICTURES). UPON INSPECTING COCKPIT DOOR LOCK, WHEN TURNED TOSep 27, 2024 · N216BZ · Airbus BD5001A11 · Air Distribution SystemSDR BAGA2023110800002Unknown · unknownUNSCHEDULED ENGINE CHANGE PERFORMED DUE TO EXCESSIVE OIL CONSUMPTION. BORESCOPE INSPECTION CONFIRMED #4 BEARING CARBON SEAL LEAK TO BE THE CAUSE. #2 RH ENGINE CONSUMED OVER OPERATIONAL LIMIT OF ENGINE OIL. 5 QT/H CONSUMED DURING ESTIMATED 10FH. ENGINE MODELNov 6, 2023 · N216BZ · Airbus BD5001A11 · Engine (Turbine/Turboprop)

STCs that may be installed · 13

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

Airframe · Airbus Canada LP BD-500-1A11